Garmin Software Version 0370.17- User Manual

Garmin Software Version 0370.17

Garmin Software Version 0370.17– User Manual, read for free online in PDF format. We hope this helps you resolve any issues you may have. If you have further questions, please contact us through the contact form.

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Table of Contents:

  • Page 3 – Garmin G1000 Cockpit Reference Guide for the DA42
  • Page 7 – RECORD OF REVISIONS; Part Number
  • Page 8 – Revision Date of Revision Affected Pages
  • Page 9 – TABLE OF CONTENTS; Section 1: System Overview
  • Page 10 – ii; Section 7: Navigation
  • Page 11 – iii; Honeywell; Section 11: Abnormal Operation
  • Page 12 – Blank Page
  • Page 13 – SECTION 1; SECTION 1: SYSTEM OVERVIEW; The purpose of this Cockpit Reference Guide is to; The pilot should read and thoroughly
  • Page 14 – MFD Only
  • Page 16 – Softkey OFF
  • Page 17 – Figure 1-3 PFD Softkey Flow Chart – 1; PFD
  • Page 18 – Figure 1-4 PFD Softkey Flow Chart – 2; OBS; Figure 1-5 PFD Softkey Flow Chart – 3; XPDR
  • Page 20 – Figure 1-6 MFD Softkeys
  • Page 21 – Figure 1-7 Page Group Icon
  • Page 22 – DATABASE UPDATES; Aviation Database Update; Figure 1-9 Database Update Prompt; ENT; Figure 1-10 Database Update Confirmation; Terrain and Obstacle Database Updates; These databases are not stored internally in the MFD; TOPO
  • Page 23 – Figure 1-11 Power-Up Splash Screen Window
  • Page 25 – SECTION 2; SECTION 2: FLIGHT INSTRUMENTS; Figure 2-1 Default PFD Information
  • Page 26 – Figure 2-2 Additional PFD Information; Next Waypoint
  • Page 27 – AIRSPEED INDICATOR; Figure 2-4 Airspeed Indicator; Speed Indication; Figure 2-5 Red Pointer at Vne; Speed Ranges; ATTITUDE INDICATOR; Figure 2-6 Attitude Indicator
  • Page 28 – Figure 2-7 Altimeter; Altitude Reference Bug; Set the Altitude Reference Bug; Altitude Trend Vector; BARO; Altitude Alerting; Figure 2-8 Altitude Alerting Visual Annunciations; Barometric Minimum Descent Altitude
  • Page 29 – Figure 2-9 Barometric Minimum Descent Altitude; INDICATOR; Figure 2-10 Marker Beacon and Vertical Deviation; VERTICAL SPEED INDICATOR; Figure 2-11 Vertical Speed Indicator; VS
  • Page 30 – HORIZONTAL SITUATION INDICATOR; Figure 2-12 Horizontal Situation Indicator
  • Page 31 – Figure 2-14 Standard-Rate Turn Indication; Course Pointer; Figure 2-15 Arc CDI and Compass Rose CDI; Bearing Pointers and Information Windows; Figure 2-16 HSI with Bearing Information
  • Page 32 – Figure 2-17 BRG1 Information Window; To display the DME Information Window, press the; Figure 2-19 DME Information Window; Navigation Source; • INTEG – GPS information is either not present or; The; Softkey is only displayed when
  • Page 33 – SECTION 3 – ENGINE; SECTION 3: ENGINE INDICATION; ENGINE; Figure 3-1 ENGINE Display; ENGINE SYSTEM DISPLAY; Figure 3-2 SYSTEM Display
  • Page 34 – If optional auxiliary fuel tanks are; If desired, use the; Fuel calculations do not use the aircraft
  • Page 35 – TRANSPONDER; The NAV/COM controls and frequency boxes are
  • Page 36 – Figure 4-2 Frequency Fields
  • Page 37 – RADIO STATUS INDICATIONS; Figure 4-5 Radio Status Indications; AUTOMATIC SQUELCH; COM; OPTIONAL NAV RADIOS; DME
  • Page 38 – Figure 4-8 Radio Tuning Window; Auto-tuning on the PFD; FMS
  • Page 39 – Figure 4-11 Ground Mode; Code Number and; Figure 4-12 Standby Mode; Manual ON Mode; ON Mode; Figure 4-14 Altitude Mode; Reply Status; Figure 4-15 Reply Indication; Reply; Code Selection; VFR Code Selection; The pre-programmed VFR Code is set at
  • Page 40 – Manual Code Entry; Following is a list of important codes:; Flight ID Reporting; If so configured, the Flight ID may be entered in the; Flight ID
  • Page 41 – SECTION 5 – AUDIO PANEL; SECTION 5: AUDIO PANEL; Figure 5-1 Audio Panel Controls
  • Page 42 – COM RADIO SELECTION; Figure 5-2 Transceivers; SPLIT COM FUNCTION; NOTE; Split COM performance is affected by; Figure 5-3 Split COM Function; MARKER BEACON RECEIVER; Figure 5-4 Marker Beacon Annunciators on the PFD
  • Page 43 – HI SENS; Figure 5-5 Marker Beacon; NAV RADIO AUDIO SELECTION; Table 5-1 ICS Isolation Modes; PILOT; Figure 5-7 ICS Isolation
  • Page 44 – INTERCOM SQUELCH CONTROL
  • Page 45 – SECTION 6 – AUTOMATIC; SECTION 6: AUTOMATIC FLIGHT; Figure 6-1 AFCS Keys; MODE ANNUNCIATIONS
  • Page 46 – Figure 6-3 PFD AFCS Display; AP; Figure 6-4 Autopilot Engaged Annunciation; Automatic Disengagement; AP DISC; Figure 6-5 Automatic Disconnect Annunciation
  • Page 47 – Figure 6-6 Manual Disconnect Annunciation; Manual Disconnect; Figure 6-7 CWS Annunciation; Control Wheel Steering; Yaw Damper; Yaw Damper is active.; Figure 6-8 Yaw Damper Active; Yaw Damper is disengaging.; Figure 6-9 Yaw Damper Disengagement; PITCH AXIS MODES; AFCS Key
  • Page 48 – Flight Director; Figure 6-11 Pitch Hold Mode; CWS
  • Page 49 – ALT; Figure 6-12 Altitude Hold Mode; If the Selected Altitude is captured during; Button after the Selected Altitude is
  • Page 50 – Figure 6-13 Vertical Speed Hold Mode
  • Page 51 – toward; FLC; Figure 6-14 Flight Level Change Mode; Altitude Hold Mode is armed.
  • Page 52 – GA; Pressing the CWS Button while Glideslope; APR
  • Page 53 – Mode annunciations for active roll axis modes are; Figure 6-16 Roll Hold Mode
  • Page 54 – Figure 6-17 Heading Select Mode; HDG
  • Page 55 – NAV; When making a backcourse approach, set; Navigation Mode Armed
  • Page 56 – Approach Mode acquires and tracks the selected; While using Approach Mode, the; See the Example Procedures Using AFCS section for
  • Page 57 – EXAMPLE PROCEDURES USING AFCS; This section provides a scenario-based set of procedures; Figure 6-20 Flight Plan Overview
  • Page 58 – Figure 6-21 Departure
  • Page 59 – Changing the HSI mode cancels; CDI; Figure 6-22 Intercepting a VOR
  • Page 60 – Figure 6-23 Transition to GPS Flight Plan
  • Page 61 – While flying the GPS leg from Panoche VORTAC to; Knob, set the Selected Altitude; Key to activate Flight Level; Figure 6-24 FLC Descent; ) Reduce power to allow descent in Flight Level
  • Page 62 – Figure 6-25 ILS Approach to KFAT
  • Page 64 – AFCS ANNUNCIATIONS AND ALERTS; AFCS Status Alerts; The following annunciations (listed in order of; Figure 6-27 AFCS Status Annunciation; AFCS Status
  • Page 65 – Overspeed protection is provided in situations where; Figure 6-28 Overspeed Annunciation; Airspeed
  • Page 67 – SECTION 7 – NAVIGATION; SECTION 7: NAVIGATION; The following discussions pertain to the Multi Function; NAVIGATION MAP PAGE; Select the MAP Page Group; The map display should only be; Direct-to Navigation from the MFD
  • Page 68 – Figure 7-3 Canceling Direct-to Navigation; Direct-to Navigation from the PFD
  • Page 69 – AIRPORT INFORMATION; Figure 7-5 Airport Information Page; Select the Airport Information Page
  • Page 70 – INTERSECTION INFORMATION; Select the Intersection Information Page; Figure 7-6 Intersection Information Page; Select the NDB Information Page
  • Page 71 – Figure 7-8 VOR Information Page; Select the VOR Information Page; USER WAYPOINT INFORMATION; See the Flight Planning section for a discussion on; NEAREST AIRPORTS; Figure 7-9 Nearest Airports Page; Nearest Airport Information on the MFD
  • Page 72 – Figure 7-10 Nearest Airports Window
  • Page 73 – NEAREST INTERSECTIONS; Figure 7-11 Nearest Intersections Page; Select the Nearest Intersections Page; Figure 7-12 Nearest NDB Page; Select the Nearest NDB Page
  • Page 74 – Figure 7-13 Nearest VOR Page; NEAREST USER WAYPOINT; Figure 7-14 Nearest User Waypoints Page; Select the Nearest User Waypoint Page
  • Page 75 – NEAREST FREQUENCIES; Figure 7-15 Nearest Frequencies Page; Select the Nearest Frequencies Page; NEAREST AIRSPACES; Figure 7-16 Nearest Airspaces Page; Select the Nearest Airspaces Page; • If the projected course takes the aircraft inside an
  • Page 77 – SECTION 8 – FLIGHT PLANNING; SECTION 8: FLIGHT PLANNING; USER DEFINED WAYPOINTS; Figure 8-1 User WPT Information Page; Select the User WPT Information Page
  • Page 78 – VIEWING THE ACTIVE FLIGHT PLAN; Figure 8-2 Active Flight Plan Window on the PFD; ACTIVATE A STORED FLIGHT PLAN; Figure 8-4 Flight Plan Catalog Page
  • Page 79 – ACTIVATE A FLIGHT PLAN LEG; Figure 8-5 Activate Flight Plan Leg Confirmation; STOP NAVIGATING A FLIGHT PLAN; Figure 8-6 Delete Flight Plan; INVERT ACTIVE FLIGHT PLAN; Figure 8-8 Invert Flight Plan
  • Page 80 – CREATE A NEW FLIGHT PLAN; Create a New Flight Plan Using the MFD; Figure 8-10 Create FPL on MFD; Create a New Flight Plan Using the PFD; A flight plan cannot be entered using the
  • Page 81 – Figure 8-13 Store Flight Plan Confirmation
  • Page 82 – INVERT AND ACTIVATE A STORED
  • Page 83 – Figure 8-15 Trip Planning Page; Starting WPT; The Page Mode must be set to MANUAL
  • Page 84 – : An active flight plan or Direct-to must be; : VNAV is advisory only and cannot be; Create a Vertical Navigation Profile
  • Page 85 – 0) With the ‘TARGET ALTITUDE’ field highlighted,; Knobs to select; Key. The cursor is now placed; MAP; VNAV Page Menu Options; MENU
  • Page 87 – SECTION 9 – PROCEDURES; SECTION 9: PROCEDURES; ARRIVALS AND DEPARTURES; Load and Activate a Departure Procedure; Figure 9-1 Select Departure; Load and Activate an Arrival Procedure; Figure 9-3 Select Arrival
  • Page 88 – Figure 9-4 Select Arrival Transition; Not all approaches in the database are approved for GPS; Load and/or Activate an Approach Procedure; Figure 9-6 Selecting an Approach Procedure
  • Page 89 – Figure 9-7 Selecting an Approach Transition; Activate an Approach in the Active Flight Plan
  • Page 91 – SECTION 10 – HAZARD; SECTION 10: HAZARD AVOIDANCE; CUSTOMIZING THE HAZARD; Figure 10-1 Page Menu
  • Page 92 – At a map range of less than 25 nm, Stormscope; Figure 10-5 Lightning Display Range Annunciation; Stormscope Page; Figure 10-6 Stormscope Page
  • Page 93 – “Cell Mode” uses a clustering program to
  • Page 94 – Figure 10-8 METAR and TAF Text Displayed on the; NEXRAD
  • Page 95 – Strikes depicted represent cloud to ground; to display the panning; Joystick; to place the panning arrow; Key to display pertinent information
  • Page 96 – Note that pressing the; Key when panning; Key and; Key; Weather Products and Symbols; Figure 10-10 depicts the symbol for each weather; Figure 10-10 Weather Product Symbols; Echo Top (Cloud Top and Echo Top Mutually Exclusive); The XM Information Page in the AUX Page Group will; The DONE Softkey on the AUX - XM; Weather Product Age; The age for each of the enabled products is displayed
  • Page 97 – Weather Product; If the G1000 is configured to use the; Displaying Traffic on the Traffic Map Page; If data is not received for a period longer than 6 seconds,; Figure 10-11 Traffic Map Page
  • Page 98 – Figure 10-12 Self Test OK Display
  • Page 99 – Figure 10-13 Traffic Map Page; Traffic Advisory; Avidyne; Refer to the Avidyne
  • Page 100 – Figure 10-15 Traffic Map Page; Displaying Traffic on the Navigation Map; TERRAIN AND OBSTACLE PROXIMITY; Terrain data is not displayed when the
  • Page 101 – Color; Figure 10-18 Obstacle Symbols and Colors; Displaying Terrain and Obstacles on the; ) With the Navigation Map displayed, press the; Softkey. Terrain and obstacle
  • Page 102 – AIRBORNE COLOR WEATHER RADAR; Weather Radar Basics; Antenna Beam Illumination; It is important to understand the concept of the; Figure 10-19 Radar Beam from 10 inch Antenna; Figure 10-19 depicts a radar beam’s characteristics.
  • Page 103 – Radar Signal Attenuation; Attenuation because of distance is due to the fact; Radar Signal Reflectivity; Precipitation; Figure 10-21 Precipitation Type and Reflectivity
  • Page 104 – Ground Returns; Figure 10-22 Angle of Incidence; A smaller incident angle gives the radar a larger
  • Page 105 – Safe Operating Distance; Figure 10-23 MPEL Boundary; Figure 10-24 Vertical Change in Radar Beam per Nautical Mile; Basic Antenna Tilt Setup
  • Page 106 – BLACK; Figure 10-25 Precipitation Intensity Levels; Thunderstorms; Steep Gradient; Figure 10-26 Cell Irregularities
  • Page 107 – Tornadoes; Operation in Weather Mode; Begin transmitting only when it; Radar Mode
  • Page 108 – MODE; YES; to select the desired map range.; VERTICAL; Softkey to
  • Page 109 – Vertically Scanning a Storm Cell; Vertical scanning of a storm cell should; Bearing Line; can also be used to adjust bearing from; Figure 10-31 Vertical Scan Display; Adjusting Antenna Tilt Angle; In order to make an accurate interpretation of a storm
  • Page 110 – Adjusting Antenna Tilt on the Horizontal Scan; can also be used to adjust tilt up; Adjusting Antenna Tilt on the Vertical Scan; can also be used to adjust tilt.; Figure 10-32 Adjusting Tilt on Vertical Scan Display; Scan Line
  • Page 111 – Adjusting Gain; Changing the gain in weather mode; Softkey to activate the cursor in; Knob to adjust the gain for the; Knob to remove the cursor.; GAIN; Softkey again to recalibrate the
  • Page 112 – Sector Scan; Figure 10-35 Selecting Sector Scan Position; Antenna Stabilization
  • Page 113 – Weather Attenuated Color Highlight (WATCHTM); While in horizontal scan mode, this feature can be used; Figure 10-37 Horizontal Scan Without WATCHTM; Areas of Attenuated
  • Page 114 – Weather Alert; Figure 10-39 Weather Alert Indications; Weather Alerts; WX ALRT; Figure 10-40 Weather Alert on PFD
  • Page 115 – A secondary use of the weather radar system is for; Ground Map; Figure 10-41 Ground Target Return Intensity Levels; Operation in Ground Map Mode
  • Page 117 – SECTION 11 – ABNORMAL; SECTION 11: ABNORMAL; REVERSIONARY MODE; Should a system detected failure occur in either display,; Normal PFD Display; Reversionary display mode can also be manually; The Airplane Flight Manual always takes
  • Page 118 – ABNORMAL COM OPERATION; When a COM tuning failure is detected by the system,; UNUSUAL ATTITUDES; The PFD will ‘declutter’ when the aircraft enters an; Figure 11-2 Extreme Pitch Indication; STORMSCOPE OPERATION WITH; If heading is lost, strikes and/or cells must be cleared
  • Page 119 – SECTION 12 – ANNUNCIATIONS; ALERTS
  • Page 120 – ALERT LEVEL DEFINITIONS
  • Page 121 – AIRCRAFT ALERTS; The following alerts are configured specifically for the; WARNING Alerts; DOOR OPEN; CAUTION Alerts; PITOT FAIL
  • Page 122 – DEICE LVL LO; Annunciation Advisory Alerts; PFD FAN FAIL; TIS Voice Alerts; The following voice alerts can be configured for ‘Male’
  • Page 123 – The following alert annunciations appear in the AFCS; Figure 12-5 AFCS System Status Annunciation; System Status Annunciation
  • Page 124 – System Annunciation
  • Page 126 – Figure 12-6 G1000 System Failure Annunciations
  • Page 127 – Message
  • Page 128 – Alerts Window Message
  • Page 131 – GEA 71 Message Advisories
  • Page 132 – GRS 77 Message Advisories
  • Page 137 – INDEX; Signal augmentation 5-3
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Integrated Flight Deck

Cockpit Reference Guide

Diamond

DA42

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Summary

Page 3 - Garmin G1000 Cockpit Reference Guide for the DA42

Garmin G1000 Cockpit Reference Guide for the DA42 Copyright © 2004-2007 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 0370.17 or later for the DA42. Some differences in operation may be observed when comparing the information in th...

Page 7 - RECORD OF REVISIONS; Part Number

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B RR-1 RECORD OF REVISIONS Part Number Change Summary 190-00406-01 Rev A Rev B Added DME capabilityAdded BRG1/BRG2 pointersChanged Airspeed Trend VectorChanged Altitude Trend VectorAdded Checklist capabilityAdded Flight ID capabilit...

Page 8 - Revision Date of Revision Affected Pages

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B RR-2 RECORD OF REVISIONS Revision Date of Revision Affected Pages Description B April, 2007 Added pages 10- 12 through 10-26 Page 12-4 Added GWX 68 Color Weather Radar Added Check Gear message

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